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gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:aircraft
|
vertical takeoff and landing aircraft
|
|
gptkbp:climate
|
1,500 °F
|
|
gptkbp:controls
|
hydromechanical control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:developer
|
gptkb:Rolls-Royce_RB.162
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engineConfiguration
|
single_spool
|
|
gptkbp:engineType
|
axial compressor
axial turbine
RB.168-1
RB.168-10
RB.168-2
RB.168-3
RB.168-4
RB.168-5
RB.168-6
RB.168-7
RB.168-8
RB.168-9
|
|
gptkbp:firstFlight
|
1960
|
|
gptkbp:fuel_capacity
|
high efficiency
0.8 lb/hp/hr
|
|
gptkbp:fuelType
|
kerosene
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce RB.168
|
|
gptkbp:inspiration
|
military applications
|
|
gptkbp:introduced
|
1960
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Harrier
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_feature
|
vertical takeoff capability
|
|
gptkbp:number_of_stages
|
8 stages
|
|
gptkbp:operationalHistory
|
used in military aviation
|
|
gptkbp:productionYears
|
1950s to 1960s
|
|
gptkbp:propulsion
|
22,000 lbf
14.67:1
|
|
gptkbp:related_engine
|
gptkb:Rolls-Royce_RB.153
Brayton_cycle
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.199
|
|
gptkbp:technology
|
vectored thrust
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:weight
|
1,500 lb
|